Impulse Response Target Study.

Abstract

The space-time integral equation approach is extended to the problem of simple aircraft shapes. The target consisted of a cylindrical fuselage, and rectangular wings, stabilizers, and rudder. Calculations were compared to measurements. The inverse scattering problem was reformulated to take advantage of direct time domain method of solution. Solutions for the sphere, sphere capped cylinder, and flat end cylinder were developed. (Author)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1977
Accession Number
ADA044801

Entities

People

  • C. L. Bennett
  • H. Mieras
  • R. Hieronymus

Organizations

  • Sperry Corporation

Tags

Communities of Interest

  • Air Platforms
  • Cyber
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Models
  • Aircrafts
  • Composite Materials
  • Computational Science
  • Computer Programs
  • Equations
  • Far Field
  • Fins
  • Frequency
  • Frequency Response
  • Geometry
  • Integral Equations
  • Inverse Scattering
  • Leading Edges
  • Measurement
  • Scattering
  • Tin

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Explosive Engineering.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)

Technology Areas

  • Space